Tribological performance of thermoplastic composites via thermally conductive material and other fillers and a process for making the composite and molded articles of the same

ABSTRACT

This thermoplastic composition and process for making articles of the same includes a thermoplastic matrix that includes a resin and filler materials wherein the filler materials includes a combination of fibers, at least one lubricant, and thermally conductive material, for improving tribological performance of thermoplastic materials. In the alternative, a thermally conductive lubricant may be substituted for the combination of the lubricant and the thermally conductive material.

This is a divisional application of application Ser. No. 09/104,959,filed Jun. 25, 1998.

TECHNICAL FIELD

This invention relates generally to thermoplastic polymers and, inparticular, to improving the tribological performance of thermoplasticpolymers via thermally conductive media and other fillers and a processfor making the same.

BACKGROUND ART

There has been a need for high performance reinforced plasticcompositions having enhanced performance capabilities, from a standpointof durability and longevity, when exposed to wear mechanisms encounteredin a typical tribological environment. Such compositions generally havea unique combination of reinforcement materials incorporated into aplastic material.

Bearing materials comprised of self-lubricating composition materialprepared from polymers have become popular in the friction andlubrication field because they are self-lubricating, rust-resistant,light in weight, easy to fabricate, relatively low in cost and verycompatible. A large percentage of conventional metal bearing membershave been gradually replaced by bearing members made from materialsusing polymers as a matrix.

An engine driveline is one example of a tribological environment wherethe use of plastic components for dynamic sealing and bearingapplications is well known. In this environment, i.e., where a sealingor bearing interface is involved, the plastic component is exposed tofriction, pressure, high temperature and lubricants. One such dynamicplastic component is a thrust washer, which is constantly subjected to acombination of varying levels of speed and load at high temperatures.Typically, a multiple of pressure and relative velocity (P*V) is used asa measure of how rigorous and demanding the application is. For example,a P*V value can range from as low as 50,000 to as high as 1,250,000, thepressure being measured in pounds/square-inch (p.s.i.) and the velocitybeing measured in feet/minute (f.p.m.). Applications having a P*Vgreater than 150,000 are generally considered to be very demanding.

When a thrust washer is used in a dynamic bearing application, iteventually fails either due to excessive wear at a given P*V, or highthermal stresses due to poor heat dissipation, e.g., “hot spotting”, orsometimes a combination of both. Thus it is very desirable that thethrust washer has a high wear resistance at a given P*V so that itperforms as a bearing, that it has good dissipation properties to avoidthermal stresses and that it has good flexibility to provide toughnessand perform as a bearing. Thrust washers are typically made fromplastics such as polyethersulphone (PES), polyamides (PA),polyaryletherketone (PAEK) and polyphenylenesulphides (PPS), to name afew. It would be advantageous to have a lower cost alternative to thePAEK-based thermoplastic bearing materials currently used in dynamicplastic components, including thrust washers.

Besides thrust washers, there are engine parts that are also exposed totribological wear mechanisms. Sleeve bearings made from plasticcompositions are constantly subjected to a harsh environment due toelevated temperatures encountered in the engine, as well as frictionalwear and lubricants. Seal rings made from plastic compositions performthe dual function of a seal and a bearing and thus require a combinationof high wear resistance and weld line strength without a significantlyhigh flexural modulus.

It is desirable to have a thermoplastic composition that has excellentwear resistance and weld line strength properties without a significantincrease in the flexural modulus. In addition, it would be desirable tohave such a thermoplastic composition that is relatively insensitive toincreases in load, has a medium for maintaining its temperature belowits glass transition temperature, and exhibits excellent chemicalresistance.

Furthermore, it is desirable to have a thermoplastic composition withthe above qualities that is available at a lower price than comparablethermoplastic bearing materials currently on the market.

The present invention is directed to overcoming one or more of theproblems set forth above.

DISCLOSURE OF THE INVENTION

In one aspect of this invention, a thermoplastic composition isdisclosed. This thermoplastic composition includes a thermoplasticmatrix that includes a resin and filler materials wherein the fillermaterials includes a combination of fibers, at least one lubricant, andthermally conductive material, for improving tribological performance ofthermoplastic materials. In the alternative, a thermally conductivelubricant may be substituted for the combination of the lubricant andthe thermally conductive material.

In another aspect of the present invention, a process for forming aproduct that functions in a tribological environment that includes thesteps of compounding and molding a thermoplastic composition including athermoplastic matrix that includes a resin and filler materials whereinthe filler materials includes a combination of fibers, at least onelubricant, and thermally conductive material, for improved tribologicalperformance of thermoplastic materials at lower cost. In an alternative,a thermally conductive lubricant may be substituted for the combinationof the lubricant and the thermally conductive material.

BRIEF DESCRIPTION OF THE DRAWINGS

For a better understanding of the present invention, reference may bemade to the accompanying drawings in which:

FIG. 1 is a graph illustrating the torque response of a preferredembodiment of the present invention during high speed, low load P*Vtesting conditions;

FIG. 2 is a graph illustrating the temperature response of the preferredembodiment during high speed, low load P*V testing conditions;

FIG. 3 is a graph illustrating the wear test results of the preferredembodiment during high speed, low load P*V testing conditions;

FIG. 4 is a graph illustrating the volumetric wear rate for thepreferred embodiment at various system temperatures;

FIG. 5 is a graph illustrating wear test results for the preferredembodiment and a known sample composite aged in 120° C. transmission oilfor 4,000 hours;

FIG. 6 is a graph illustrating wear test results for the preferredembodiment and a known sample composite aged in 120° C. air for 4,000hours;

FIG. 7 is a graph illustrating wear test results for the preferredembodiment and a known sample composite aged in 20° C. kerosene for2,000 hours;

FIG. 8 is a graph illustrating wear test results for the preferredembodiment and a known sample composite aged in 20° C. water for 100hours;

FIG. 9 is a graph illustrating a comparison of the tensile strength andtensile elongation of the preferred embodiment and a known samplecomposite;

FIG. 10 is a graph illustrating a comparison of the flexural strengthand flexural modulus of the preferred embodiment and a known samplecomposite;

FIG. 11 is a graph illustrating the preferred embodiment's retention oftensile strength and tensile elongation after aging in 12° C.transmission fluid for 2000 hours;

FIG. 12 is a graph illustrating the preferred embodiment's retention oftensile strength and tensile elongation after aging in 120° C. air for4,000 hours;

FIG. 13 is a graph illustrating the preferred embodiment's retention oftensile strength and tensile elongation after aging in 20° C. water for500 hours;

FIG. 14 is a graph illustrating the preferred embodiment's retention oftensile strength and tensile elongation after aging in 20° C. kerosenefor 500 hours;

FIG. 15 is a graph illustrating the preferred embodiment's retention offlexural strength and flexural modulus after aging in 120° C.transmission fluid for 2,000 hours;

FIG. 16 is a graph illustrating the preferred embodiment's retention offlexural strength and flexural modulus after aging in 120° C. air for4,000 hours;

FIG. 17 is a graph illustrating the preferred embodiment's retention offlexural strength and flexural modulus after aging in 20° C. water for500 hours; and

FIG. 18 is a graph illustrating the preferred embodiment's retention offlexural strength and flexural modulus after aging in 20° C. kerosenefor 500 hours.

BEST MODE FOR CARRYING OUT THE INVENTION

In the preferred embodiment of the present invention, a combination offibers, at least one lubricant, and thermally conductive material isincorporated into a thermoplastic matrix, resulting in a reinforcedthermoplastic composition material for forming molded and extrudedproducts that function in a tribological environment. A thermallyconductive lubricant can be substituted for the combination of at leastone lubricant and thermally conductive material.

The thermoplastic matrix that holds the solid lubricants and reinforcedfibers includes a resin. This resin is preferably semi-crystalline. Thethermoplastic composition has a glass transition temperature thattypically, but not necessarily, exceeds a bulk system temperature of thesurfaces of mating components in a tribological environment, in theabsence of frictional heating. Preferably, the glass transitiontemperature is at least 70° C., advantageously over 90° C., andpreferably about 125° C.

One suitable base resin material is a thermoplastic copolymer of analiphatic-aromatic polyamide and a terephthalic aromatic chain having atrade name “Zytel HTN FE8200.” Zytel HTN FE8200 is a semi-crystallineengineering resin manufactured by E. I. du Pont de Nemours and Company,which has its corporate headquarters at 1007 Market Street, Wilmington,Del. 19898. In addition, Zytel HTN FE8200 has a glass transitiontemperature of 125° C. and a melting point of 300° C. Zytel HTN FE8200also has a higher melting point, a higher glass transition temperature,and a higher tensile strength than many other polyamide resins or higherperformance polymers. Furthermore, Zytel HTN FE8200 is a member of thenylon family and has the CAS Registry number 153148-85-4. Nylons displaya low coefficient of friction when they contact many other materials.Also, when used within their P*V limitations, nylons have goodresistance to wear. It is well known in the art that this base resin canbe filled with long glass reinforcement for use in high temperature andstructural applications. However, the preferred embodimentadvantageously uses non-glass-filled Zytel HTN FE8200 as the matrix fora bearing material.

The base resin material present in the thermoplastic compositionpreferably comprises from about 50% to about 95% by weight of thethermoplastic composition with the optimal value being about 75%.

The thermoplastic matrix may also be comprised of the base resin ofpolyphthalamide. For example, polyphthalamide is a semi-crystallineresin that has a glass transition temperature of 105° C. and a meltingpoint of 310° C. Grades of polyphthalamide provide significantlyimproved toughness comparable to other polymers and retain much higherstrength and stiffness across a broad humidity and temperature range.

Yet another base resin material that the thermoplastic matrix mayinclude is polyphenylene sulfide. Polyphenylene sulfide is a specialtyengineering plastic recognized for its unique combination of properties,including thermal stability and chemical resistance. Polyphenylenesulfide has a glass transition temperature of 85° C. and a melting pointof 285° C.

Other resins with relatively high glass transition temperatures may alsobe used for the thermoplastic matrix. Any resin, however, must have atleast a glass transition temperature that exceeds a bulk systemtemperature of the surrounding tribological environment. For example,Nylon 4, 6, which has a glass transition temperature of 82° C., andliquid crystal polymers are two additional base resins which thethermoplastic matrix may comprise.

The filler material contained in the thermoplastic matrix can include acombination of fibers, to impart an optimum combination of desirableproperties such as wear resistance and compressive strength withoutsignificant increase in flexural modulus, and lubricants to impart therequired amounts of lubricity to the thermoplastic.

In a preferred embodiment of the present invention, the fiber used inthe filler material is milled glass fiber. Using milled glass fiber isadvantageous because it conveniently has many exposed fiber ends and asmall percentage of milled glass fiber imparts a significant amount ofwear resistance. Milled glass fiber also advantageously serves tomoderately “machine” a mating surface.

The milled glass fiber used to carry out a preferred embodiment of thepresent invention has the trade name Fiberglas® brand milled fibers497DB and is manufactured by Owens Corning, that has its headquarterslocated at One Owens Corning Parkway, Toledo, Ohio 43659.

Fibers are present in the thermoplastic matrix, preferably comprising ina range from about 0% to about 35% of the thermoplastic composition withthe most preferred value being 5%. Furthermore, the fibers have a lengthdesirably in the range from about 50 to about 2500 micrometers, adiameter in the range from about 50 to about 200 micrometers, and alength to diameter ratio of about 1:20.

Numerous other fibers or fiber-like substances may be utilized,including but not limited to, glass, aramid, carbon, and ceramic.

Certain lubricants are advantageously added to the thermoplastic matrixof the embodiment to impact the required amount of lubricity to thecomposition. Some preferred lubricants include polytetrafluoroethylene,silicone resin modifier, and metallic particles. The preferred type ofmetallic particles are bronze flakes.

Polytetrafluoroethylene advantageously imparts lubricity to thethermoplastic composition and is present in the thermoplastic matrix,preferably comprising in a range from about 0% to about 20% by weight ofthe thermoplastic composition, with the most preferred value being 5%.The polytetrafluoroethylene used in carrying out a preferred embodimenthas the trade name WHITCOM PTFE TL-5, is manufactured by ICIFluropolymers and is well known in the art as a common ingredient inself-lubricated thermoplastic bearing compositions. ICI has an addressat 1300 Connecticut Avenue N.W., Suite 901, Washington D.C. 20036.

Silicone resin modifiers are known as a processing aid to be used withlow temperature resins. However, a preferred embodiment of the presentinvention advantageously utilizes an unusually higher percentage ofsilicone resin modifier as a composition bearing additive. Siliconeresin modifier conveniently imparts lubricity, aids in processing, andgives the thermoplastic flame retardance. A preferred silicone resinmodifier has the trade name Silicone Resin Modifier 4-7051, ismanufactured by Dow Corning, located at 2200 W. Salzburg Road, MidlandMich. 48686, and is present in the thermoplastic matrix, preferablycomprising from about 0% to about 20% by weight of the thermoplasticcomposition, with the most preferred value being 5%.

Metallic particles are known for use in sinterable fluoropolymercompositions as a thermally conductive agent. A preferred embodiment ofthe present invention synergistically uses bronze flakes to channel heatgenerated at the interface through the bearing and also to impartlubricity. The bronze flake used to carry out a preferred embodiment hasa trade name Bronze Flake 9020, is manufactured by Reade AdvancedMaterials. Reade Advanced Materials has an address at Post Office Drawer15039, Riverside, Rhode Island 02915-0039. Metallic particles arepresent in the thermoplastic matrix, preferably comprising in a rangefrom about 2% to about 30% by weight of the thermoplastic composition,with the most preferred value being 10%. The size of the metallicparticles can range from 0.01 micrometers to about 50 micrometers withthe optimal size of around 12.57 micrometers.

Tribological performance data for the thermoplastic composition bearingmaterial of a preferred embodiment of the present invention is shown inFIGS. 1 and 2. FIG. 1 shows the torque response for the embodiment. TheP*V is varied by changing the speed and load inputs. The approximate P*Vlevels for each step are shown at the bottom of the graph, ranging from100,000 p.s.i.*f.p.m. to 300,000 p.s.i.*f.p.m. Input speed and load, aredenoted as high, medium, and low. The resultant torque reading for thesystem is shown by a star for known samples and by a circle for thepreferred embodiment of the present invention.

FIG. 1 shows that the present invention is much more insensitive toincreases in load than the known samples. Furthermore, even as thelubricant film is squeezed out at higher loads, the lubricity of thecomposition does not allow a significant increase in the coefficient offriction.

FIG. 2 shows the temperature response of the thermoplastic composition.Input speed and load, denoted by high, medium, and low are listed alongthe x-axis. The resultant average interfacial temperature reading forthe system is shown by a star for a known sample and by a circle for thepreferred embodiment of the present invention. Also, as shown in FIG. 2,the average interfacial temperature remains below 120° C. because thereis no appreciable increase in the coefficient of friction. However, evenif the coefficient of friction were to rise at high loads, higher thanthat shown in FIG. 2, the thermal conductivity of the resin wouldadvantageously help function as a means to channel the heat away fromthe interface and delay the onset of accelerated wear.

In a test where the splash lubricant was removed and the load wascontinually increased, the interface temperature of a PAEK-basedthermoplastic bearing material increased past its glass transitiontemperature and caused failure within twenty-four minutes. However,under the same conditions, a preferred embodiment of the presentinvention lasted for almost two hours before system failure. Thisdemonstrates the superior performance of the present invention.

Testing was also conducted to determine the P*V capability of apreferred embodiment at a constant speed of 1800 rpm, while continuallyincreasing load. This test showed that the PAEK-based bearing materialexhibited catastrophic interface temperatures at a pressure of 300p.s.i., resulting in a P*V limit of 336,000 p.s.i.*f.p.m. under theseconditions. The preferred embodiment tested showed no appreciableincrease in interface temperature up to a pressure of 500 p.s.i., (thelimit of the test) resulting in a P*V capability of at least 560,000p.s.i.*f.p.m. under the conditions tested. This confirms the superiorperformance of the preferred embodiment.

Wear tests were also conducted to determine the wear resistance of apreferred embodiment of the present invention. FIG. 3 shows a comparisonof the embodiment's wear depth, compared to that of other more expensiveplastic bearing materials after a 100 hour wear test conducted at a p*vof 205,000 p.s.i.*f.p.m. under splash lubricated conditions. As shown onFIG. 3, the wear test shows that the preferred embodiment meets thepre-set requirement that it performs at least as well as other, moreexpensive transmission thrust washer materials, with the sole exceptionof a composition formed of a self-lubricated, PAEK-based thermoplasticbearing material. However, the performance of the preferred embodimentis nearly as good as that of that of the self-lubricated, PAEK-basedthermoplastic bearing material.

The preferred embodiment of the present invention is also lubriciousenough to prevent detrimental frictional heat in lubricated tribologicalcontacts at normal system temperatures in the range of 70° C. to 100° C.However, because heat may evolve in a transmission from an externalsource, testing was conducted to determine the tribological response atexcessive system temperatures. Upon completion of a test run at a systemtemperature of 132° C., the known sample composition showed catastrophicfailure due to melting at a P*V level in the range from about 392,000 toabout 448,000 p.s.i.*f.p.m. The preferred embodiment tested under thesame conditions, does not show any signs of melting. Furthermore, thewear depth for the sample thrust washer comprised of the preferredembodiment had a wear depth of only 0.017 millimeters.

Additional testing was performed by exposing a washer made from apreferred embodiment of the present invention to a 132° C. oil deliverytemperature at 205,000 P*V for 100 hours. The resulting wear rate of0.00263 cubic centimeters per hour (cm³/hr) indicates that the samplecould run for over 800 hours at these conditions. The volumetric wearrate for the present invention at various system temperatures is shownin FIG. 4.

For a preferred embodiment of the present invention having a nylon-basedcopolymer base resin, testing was necessary to evaluate the potentialeffect of aging on physical and tribological properties. A typicalexample of a tribological component is, but is not limited to, atransmission thrust washer. A transmission thrust washer is commonlyexposed to hot air and transmission oil, and could also be exposed towater and kerosene. Therefore, testing was conducted to see how thenylon-based copolymer would perform when exposed to these conditionsover time. Tribological results from a 4,000 hour aging test, comparingthe wear of the embodiment to the wear of the known sample composition,are shown in FIGS. 5-8.

FIG. 5 shows the wear test results for samples of a preferred embodimentof the present invention aged in 120° C. transmission oil for 4,000hours. FIG. 6 shows the wear test results for samples aged in 120° C.air for 4000 hours. FIG. 7 shows the wear test results for samples agedin 20° C. Kerosene for 2,000 hours. FIG. 8 shows the wear test resultsfor samples aged in 20° C. water for 100 hours. The results from thetests, as reflected in FIGS. 5-8, demonstrate the preferred embodiment'sexcellent chemical resistance and its superior performance over time,when subjected to adverse operating conditions.

The preferred embodiment of the present invention also exhibits superiorweld line strength. Weld line strength can be described as a measure ofthe flexural strength of a thrust washer across its weld line. It isoften expressed as a percent of parent material and designated as weldline strength retention. The preferred embodiment of the presentinvention exhibits a weld line strength retention of over 90%, which isconsidered excellent. Weld line strength is important because if thewasher were to break in a transmission, it would be much more likely tofall from the gear-carrier interface and cause excessive wear betweenthe gear and the carrier as well as other transmission problems.

The physical properties for bearing materials used in thrust washersneed to be of adequate strength to support the compressive loading onthe washers and to withstand the minimum flexing due to a wavy matingsurface. FIG. 9 compares the tensile strength and tensile elongation ofa preferred embodiment of the present invention with that of the knownsample composition. FIG. 10 compares the flexural strength and flexuralmodulus of the preferred embodiment with that of the known samplecomposition. Those skilled in the art can see from FIGS. 9 and 10 thatthe preferred embodiment's tensile strength and flexural strength aremore than adequate for most bearing applications.

It is well known in the art that aging samples and noting their physicalproperty retention after their exposure to particular fluids over timeis beneficial. Normally, if physical properties are retained at levelsof 90% or better, the material's resistance to chemical attack underthose conditions would be considered excellent. A preferred embodimentof the present invention was tested by aging in hot transmission oil,hot air, kerosene and water for up to 4,000 hours.

The tensile properties of a preferred embodiment of the presentinvention at various time intervals are shown in FIGS. 11-14. FIG. 11 isa graph illustrating the preferred embodiment's retention of tensilestrength and tensile elongation after aging in 120° C. transmissionfluid for 2000 hours. FIG. 12 is a graph illustrating the preferredembodiment's retention of tensile strength and tensile elongation afteraging in 120° C. air for 4,000 hours. FIG. 13 is a graph illustratingthe preferred embodiment's retention of tensile strength and tensileelongation after aging in 20° C. water for 500 hours. FIG. 14 is a graphillustrating the preferred embodiment's retention of tensile strengthand tensile elongation after aging in 20° C. kerosene for 500 hours. Asseen in FIGS. 11-14, the preferred embodiment showed excellent chemicalresistance under these conditions, retaining its tensile properties at alevel above 90% under each of the testing conditions.

The flexural properties of a preferred embodiment at various timeintervals are shown in FIGS. 15-18. FIG. 15 is a graph illustrating theretention of flexural strength and flexural modulus after aging in 120°C. transmission fluid for 2,000 hours. FIG. 16 is a graph illustratingthe retention of flexural strength and flexural modulus after aging in120° C. air for 4,000 hours. FIG. 17 is a graph illustrating theretention of flexural strength and flexural modulus after aging in 20°C. water for 500 hours. FIG. 18 is a graph illustrating the retention offlexural strength and flexural modulus after aging in 20° C. kerosenefor 500 hours. Under each testing condition, all flexural propertieswere maintained at levels above 90%, with one exception. When exposed to120° C. air for 4000 hours, the preferred embodiment of the presentinvention showed only a 70% retention of its flexural strength. This, incombination with the sample's failure mode, indicates that the materialwas becoming slightly more brittle. It is unlikely that the materialwould become more brittle upon further exposure to hot air. Furthermore,the flexural property retention was still in an acceptable range, asthrust washers do not see much flex in their application and thetribological properties of the present invention do not catastrophicallyworsen under these conditions.

Industrial Applicability

The present invention is a thermoplastic composition that isadvantageously applicable in a tribological environment. Thethermoplastic composition according to the present invention can beuseful in a variety of applications where a combination of wearresistance and weld line strength is desirable without a significantincrease in the flexural modulus. Furthermore, the present embodiment isuseful for high performance plastic components in applications where asealing or bearing interface is involved and where the plastic componentis exposed to friction, pressure, high temperature and lubricants. Thus,the present embodiment is particularly useful for making thrust washers,pump seals, sleeve bearings and other dynamic bearing and sealingcomponents for engines and transmissions.

Also, the raw material cost of the preferred embodiment of the presentinvention is significantly lower than the raw material cost of thethermoplastic bearing materials well known in the art for similar andidentical applications.

The following description is only for the purposes of illustration andis not intended to limit the present invention as such. It will berecognizable, by those skilled in the art, that the present invention issuitable for a plurality of other applications.

In view of the foregoing, it is readily apparent that the subjectthermoplastic composition provides a superior and cost-effectivematerial that very effectively functions within a tribologicalenvironment.

Other aspects, objects and advantages of the present invention can beobtained from a study of the drawings, the disclosure and the appendedclaims.

What is claimed is:
 1. A process for forming a product that functions ina tribological environment comprising the steps of: compounding athermoplastic composition including a thermoplastic matrix that includes(i) the substance having the CAS Registry Number 253148-84-4 and (ii)filler materials wherein said filler materials includes a combination offibers, at least one lubricant, and thermally conductive material, forimproving tribological performance of thermoplastic materials; andmolding said compounded thermoplastic composition into a product.
 2. Theprocess for forming a product according to claim 1, wherein saidthermoplastic composition has a glass transition temperature thatexceeds a bulk system temperature of surfaces of mating components in atribological environment, in the absence of frictional heating.
 3. Theprocess for forming a product according to claim 1, wherein said step ofcompounding includes said step of compounding includes single screwextrusion.
 4. The process for forming a product according to claim 1,wherein said step of compounding includes twin screw extrusion.
 5. Theprocess for forming a product according to claim 1, wherein said step ofcompounding includes batch mixing.
 6. The process for forming a productaccording to claim 1, wherein said step of molding includes injectionmolding.
 7. The process for forming a product according to claim 1,wherein said step of molding includes compression molding.
 8. Theprocess for forming a product according to claim 1, wherein said step ofmolding includes extrusion molding.
 9. The process for forming a productaccording to claim 1, wherein said steps of compounding and molding areperformed simultaneously.
 10. The process for forming a productaccording to claim 1, wherein said lubricant includespolytetrafluoroethylene.
 11. The process for forming a product accordingto claim 1, wherein said lubricant includes silicone resin modifier. 12.The process for forming a product according to claim 1, wherein saidthermally conductive material includes metallic particles.
 13. Theprocess for forming a product according to claim 1, wherein said fibersare selected from a group that includes glass, aramid, carbon, andceramic.
 14. The process for forming a product according to claim 1,wherein said resin is semi-crystalline.
 15. A process for forming aproduct that functions in a tribological environment comprising thesteps of: compounding a thermoplastic composition including athermoplastic matrix that includes (i) the substance having the CASRegistry Number 253148-84-4 and (ii) filler materials wherein saidfiller materials includes a combination of fibers and a thermallyconductive lubricant, for improving tribological performance ofthermoplastic materials; and molding said compounded thermoplasticcomposition into a product.
 16. The process for forming a productaccording to claim 15, wherein said thermoplastic composition has aglass transition temperature that exceeds a bulk system temperature ofsurfaces of mating components in a tribological environment, in theabsence of frictional heating.
 17. The process for forming a productaccording to claim 15, wherein said step of compounding includes singlescrew extrusion.
 18. The process for forming a product according toclaim 15, wherein said step of compounding includes twin screwextrusion.
 19. The process for forming a product according to claim 15,wherein said step of compounding includes batch mixing.
 20. The processfor forming a product according to claim 15, wherein said step ofmolding includes injection molding.
 21. The process for forming aproduct according to claim 15, wherein said step of molding includescompression molding.
 22. The process for forming a product according toclaim 15, wherein said step of molding includes extrusion molding. 23.The process for forming a product according to claim 15, wherein saidsteps of compounding and molding are performed simultaneously.
 24. Theprocess for forming a product according to claim 15, wherein saidthermally conductive lubricant is selected from a group that includesconductive ceramics and metallic particles.
 25. The process for forminga product according to claim 15, wherein said fibers are selected from agroup that includes glass, aramid, carbon, and ceramic.
 26. The processfor forming a product according to claim 15, wherein said resin issemi-crystalline.